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IM2830AJ.doc
IM2830A
Directory: 962830A
Rev: J
Shadin Avionics
INSTALLATION MANUAL
FUEL/AIR DATA COMPUTER
Sec: VII
P/N 962830A-1(A), 962830A-2(A), 962830A-3(A)
Page i of vi
PAGE CONTROL CHART
SECTION
NO.
1.0
2.0
DESCRIPTION
PAGE
REVISION LOG
vi
OVERVIEW
1-1
1.1
1.2
1.3
1.4
1.5
1-1
1-1
1-2
1-3
1-3
The Manual
Product Information
System Configuration
Fuel Totalizer Configuration
F/ADC2000, Argus Moving Map Configuration
FUEL AND AIR DATA SYSTEM SPECIFICATIONS
2-1
2.1
2.2
2-1
2-1
2-2
2-2
2-3
2-4
2-5
2-5
2-5
2-5
2-6
2-6
2-7
2-8
2-8
2-8
2-8
2-9
2-10
2-11
2-12
2-13
2-14
2-14
2-14
2-14
2-15
2-15
2-15
2-16
2-16
2.3
2.4
2.5
2.6
2.7
2.8
2.9
Input Data Range
Output Data Range
Table 1 – Calibrated Airspeed Tolerance
Table 2 – Pressure Altitude Tolerance
Table 3 – Vertical Airspeed Tolerance
Table 4 – MACH Tolerance
Dimensions
Power Requirements
Output Data
2.5.1 Serial Output Data Parameters
2.5.2 ARINC 429 Labels Associated with Switch Settings
Table 5 – ARINC Label Configuration
2.5.3 ARINC 429 Labels Associated with Switch Settings
Limitations
2.6.1 Warm-up Time
2.6.2 Supplemental Equipment
2.6.3 Static/Pitot Source Error Correction (SSEC/PSEC)
2.6.4 SSEC/PSEC Listing
2.6.4 SSEC/PSEC Listing (Continued)
2.6.4 SSEC/PSEC Listing (Continued)
2.6.4 SSEC/PSEC Listing (Continued)
Part Numbering Scheme
Electrical Interface Specifications
2.8.1 Heading Interface
2.8.2 Fuel Flow Interfaces
2.8.2.1 Digital Fuel Flow
2.8.2.2 Sine Wave Fuel Flow
2.8.2.3 DC Voltage Fuel Flow
2.8.3 Baro Interface
Statistical Specifications
2.9.1 Mean Time Between Failures